Nonlinear response functions of the burning rate of RDX and HMX

Author:

Zenin A. A.,Finjakov S. V.

Publisher

Pleiades Publishing Ltd

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference49 articles.

1. F. T. C. Culick, “Combustion Instabilities: Mating Dance of Chemical, Combustion, and Combustors Dynamics,” AIAA Paper No. 2000-3178, (2000).

2. C. M. Mihlfeith, A. D. Baer, and N. W. Ryan, “The Response of a Burning Propellant Surface to Thermal Radiation,” AIAA J. 10(10), 1280–1285 (1972).

3. J. C. Finlinson, D. Hanson-Parr, S. F. Son, and M. Q. Brewster, “Measurement of Propellant Combustion Response to Sinusoidal Radiant Heat Flux,” AIAA Paper No. 91-0204, 1991.

4. V. E. Zarko, V. N. Simonenko, and A. B. Kiskin, “Radiation Driven Transient Burning,” in Progress in Astronautics and Aeronautics, Vol. 143: Nonsteady Burning and Combustion Stability of Solid-Propellants, Ed. by L. De Luca, E. W. Price, M. Summerfield (AIAA, Washington 1992), pp. 363–398.

5. T. A. Litzinger, C. J. Tang, G. Kudra, and Y. J. Lee, “A Study of the Combustion Response of HMX Monopropellant to Sinusoidal Laser Heating,” in 33rd JANNAF Combustion Meeting, Vol. II (CPIA Publ. 653, 1996), pp. 159–168.

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1. Hot-Spot Combustion of HMX;Russian Journal of Physical Chemistry B;2023-04

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